DocumentCode :
1474824
Title :
Helix antenna for spacecraft
Author :
Das, Allen
Author_Institution :
TRW Systems, Redondo Beach, USA
Volume :
37
Issue :
4
fYear :
1969
fDate :
4/1/1969 12:00:00 AM
Firstpage :
237
Lastpage :
240
Abstract :
This paper describes the development and performance of a light-weight, high-gain, high-efficiency, rigid helix antenna and discusses a light-weight deployable helix antenna. The weight of the rigid helix was 016 kg (0.35 lb) and had a measured gain of 16.5 dB at 2.3 GHz. The estimated weight of the deployable helix is 0.06 kg (0.13 lb). Such antenna elements can be used for phased arrays for spacecraft.
Keywords :
antenna arrays; dipole antennas; space communication links; space vehicles;
fLanguage :
English
Journal_Title :
Radio and Electronic Engineer
Publisher :
iet
ISSN :
0033-7722
Type :
jour
DOI :
10.1049/ree.1969.0042
Filename :
5267281
Link To Document :
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